|Publication number||US7304814 B2|
|Application number||US 11/444,051|
|Publication date||Dec 4, 2007|
|Filing date||May 31, 2006|
|Priority date||Jun 22, 2004|
|Also published as||CN1712938A, CN100570334C, US7075082, US7609463, US20050279941, US20060215166, US20080297902, WO2006007344A2, WO2006007344A3|
|Publication number||11444051, 444051, US 7304814 B2, US 7304814B2, US-B2-7304814, US7304814 B2, US7304814B2|
|Original Assignee||Wilmington Infrared Technologies, Inc.|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (37), Non-Patent Citations (39), Referenced by (6), Classifications (22), Legal Events (4)|
|External Links: USPTO, USPTO Assignment, Espacenet|
The present application is a divisional of U.S. patent application Ser. No. 10/873,780, filed Jun. 22, 2004 now U.S. Pat. No. 7,075,082, entitled “Compact Infrared Spectrometer, And Methods And Systems For Manufacture And Assembly Of Components Used In Same,” the contents of which are incorporated herein in their entirety by reference.
The present relates to infrared spectrometers, and also to systems and methods for manufacturing and assembling optical components including components that may be used in infrared spectrometers.
Infrared spectroscopy had its origin when William Herschel discovered optical radiation beyond the red portion of the visible spectrum, which had been discovered by Isaac Newton. Since the 19th century, the interaction between infrared radiation and different substances had been studied by scholars in the fields of both physics and chemistry. It has since been found that different materials absorb different portions of the infrared spectrum and these absorption features can be used to detect and identify chemical species. The first mass-produced infrared spectrometer was not built until World War II, when the US Office of Rubber Reserve identified the use of infrared spectroscopy as an effective means for measuring the compositions of the synthetic rubber compounds, and demanded the development of infrared spectrometers capable of operation from 1 μm and beyond. Since 1950, infrared spectrometers have gained wide acceptance by both the scientific and engineering communities. The first generation of these spectrometers utilized the optical dispersion of infrared radiation by rock salt materials such as sodium chloride (NaCl). Later these hygroscopic, or moisture-sensitive, rock salt prisms were replaced by diffractive gratings made with glass substrates. In general, these early infrared spectrometers weighed over 200 pounds, and were packaged in a space larger than 7 to 8 cubic feet in volume.
In addition to the dispersion-based infrared spectrometers, in late 1960s, with the advancements in lasers, computers and data storage devices, a new type of infrared spectrometer based on the principle of optical interferometry, was developed. Due to the computation involved in converting the interferometric measurements to optical spectra by the mathematical calculation of Fourier Transformation, these infrared instruments are also known in the infrared spectroscopy art as FTIR. Despite the fact that these FTIR spectrometers have provided highly improved sensitivity and spectral resolution compared to the dispersive infrared spectrometers, the interferometric nature of these instruments requires that ultimate environmental control be observed during their operation. This is because the interferometric measurements require the overlapping of two optical beams within the distance of half a wavelength, i.e., a precision in the micrometer range. In other words, any minute changes in the temperature or any small amount of vibration would result in failure to obtain useable spectra from such an FTIR spectrometer. Due to the incorporation of the optical interferometer and all the related feedback and control electronics, an FTIR usually weighs from 150 to 400 pounds and occupies a volume of 3 to 10 cubic feet.
For many modern industrial, security and military tasks, the abilities to detect the infrared spectral signatures of chemicals on the surface or in the atmosphere is highly valuable. These types of chemical information often can be used to determine the quality of a production process, or to evaluate the danger to approach or enter an area. However, due to the limitations in size, weight and ruggedness, infrared spectrometers have not been widely used as a first-line detection or monitoring tools for these applications, but rather as an off-line or laboratory validation tool.
To alleviate the practical limitations mentioned above, it would be desirable to develop a sensitive, light-weight, rugged and compact infrared spectrometer capable of detecting and/or identifying different chemical species under hostile service conditions. To achieve these goals, a compact optical spectrometer design is needed to cover a wide range of the infrared wavelengths, especially one that falls into the so-called “infrared fingerprint” (7-14 μm) region. This is because the infrared absorption features in the fingerprint region will provide the most distinctive chemical evidence that can be used to identify different substances.
While it could be straightforward to use the principles behind an FTIR to build smaller spectrometers that cover a wide range of the infrared spectrum, the low resistance to environmental changes may not meet the ruggedness requirements for field applications.
Another consideration related to the economics of the instrument is the ease of assembly. Inside all the infrared spectrometers today, the majority of the optical components found are made of glass materials. Whether it is the grating in a dispersive instrument or the mirrors within an FTIR, these glass-based components are often glued or clamped to mounts before they can be secured and then aligned. The accuracy of the gluing process, the possible shrinkage of the glue or epoxy and the chipping of the glass edges, all place uncertainties on the precision of the final alignment. As a result, these instruments need frequent maintenance or alignment after leaving the assembly line. Even during the assembly process, highly skilled opticians are required for proper alignment of all of these optical components, making the production more costly. The present invention provides a solution to these and other shortcomings found in the prior art.
In the present invention, a dispersive infrared spectrometer has been designed to work in tandem with two-dimensional infrared detectors. By tightly packing the optical paths within the spectrometer and carefully maintaining the divergence and convergence of the optical beams, the present invention achieves compactness while at the same time produces a focused infrared spectrograph on a two-dimensional detector which covers 4.5 or more microns of the infrared spectrum.
To further enhance the ruggedness of the spectrometer, all optical components and their mounting fixtures are fabricated from metals rather than glass, making the resulting spectrometer highly resistant to shocks and vibrations. Also, being dispersive rather than interferometric in its working principle, the spectrometer is significantly less vulnerable to the environmental changes.
In order to improve the ease of assembly and maintenance on such an infrared spectrometer, a push-and-lock mounting scheme is designed for optical components and component modules in this spectrometer. This simplifies the assembling process and at the same time achieves permanent alignment without the use of welding, brazing or gluing. In one embodiment, the assembly method does not require sophisticated optical testing for quality control purposes during the assembling process and is therefore more cost-effective. Finally, due to the rugged design and the permanent alignment, the spectrometer requires minimal maintenance once it is deployed, making it a more effective tool for field applications found in factories, public areas and battle fields. In one embodiment, the present invention is directed to a compact spectrometer operable in a wavelength range of 4.5 or more microns (preferably 7.5 to 13.5 microns or 4.5 or more microns within the 7.5 to 13.5 micron range). The spectrometer includes an entrance slit, a collimating mirror, a grating, a focusing mirror and a first focal plane. At least some radiation passing through the slit follows an optical path in which at least some radiation passing through the slit is reflected by the collimating mirror onto the grating, which in turn reflects at least some radiation onto the focusing mirror, which in turn reflects and focuses at least some radiation at a first focal plane and onto the two-dimensional array of detectors (which may be located at the first focal plane or another focal plane.) Each column in the two-dimensional array of detectors corresponds to a portion of the 4.5 or more micron range, the two-dimensional array includes a plurality of columns that collectively correspond to wavelengths spanning the 4.5 or more micron range, and each adjacent pair of columns in the two-dimensional array of detectors may correspond to wavelengths that differ by an equal amount. The entrance slit, the collimating mirror, the grating, the focusing mirror and the first focal plane are positioned within a volume that is equal or less than 192 cubic inches in size, and preferably satisfy some or all of the following design requirements:
1. Spacing among the components should be tightly arranged, yet cross-talk, undesired reflection or transmission and/or scattering should be reduced or eliminated;
2. The spatial and angular arrangement of the components should produce the desired wavelength coverage (on the detector array) without excessive aberration, such as spherical aberration, coma, astigmatism or chromatic aberration, and without excessive loss of the infrared energy passing through the slit;
3. In embodiments where the detector array (or infrared camera) is situated at a second focal plane (different from the first focal plane), the arrangement of the components preferably allows the infrared spectrum focused at the first focal plane (spectrograph) to be conveniently and efficiently relayed and refocused onto the two-dimensional array of detectors (or infrared camera) at the second focal plane;
4. The focused spectrum preferably utilizes the entire width of the two-dimensional detector array detector so that the spectral resolution is maximized; and
5. The height of the focused spectrum on the two-dimensional detector array is preferably maximized with minimal or no distortion so that a vertical average of pixels on the detector array (corresponding to the same wavelength) may be taken, or “binned”, to enhance the signal-to-noise performance.
In accordance with a further aspect, the present invention is directed to a method for aligning and coupling an optical component to a substrate with a precision of at least 12.5 microns in position and 0.075 degrees in angular orientation. An optical component is machined from a material selected from aluminum, aluminum alloys, stainless steel, nickel, copper or beryllium. The optical component is affixed to a mount having a flat bottom surface that defines a first plane. A cylindrical rod extends away from the flat bottom surface of the mount at an angle perpendicular to the first plane, and at least first and second screws are disposed in first and second cylindrical openings that extend through the bottom surface of the mount. The first and second cylindrical openings in the mount are aligned perpendicular to the first plane and have an inner diameter that matches an outer diameter of the first and second screws. A substrate is provided having a flat upper surface that defines a second plane, wherein a first cylindrical opening extends from the upper surface of the substrate into the substrate at an angle perpendicular to the second plane, and wherein at least second and third threaded openings extend from the upper surface of the substrate into the substrate at an angle perpendicular to the second plane. The mount is positioned with respect to the substrate by simultaneously aligning the metal rod with the first opening in the substrate, the first opening in the mount with the second threaded opening in the substrate, and the second opening in the mount with the third threaded opening in the substrate. While the mount and the substrate are aligned, the cylindrical rod is inserted into the first cylindrical opening in the substrate until the bottom surface of the mount contacts the upper surface of the substrate. Following the inserting, friction between the cylindrical rod and the first opening in the substrate inhibits rotation of the mount about an axis perpendicular to the first and second planes, and tightness between the first opening in the substrate and the cylindrical rod restricts lateral movement of the mount with respect to the substrate. After the inserting, the first and second screws are rotated into the second and third threaded openings respectively in the substrate, whereby the mount is coupled to the substrate with said precision (i.e., at least 12.5 microns in position and 0.075 degrees in angular orientation.)
In accordance with a still further aspect, the present invention is directed to a method for aligning and coupling an optical component to a mount with a precision of at least 12.5 microns in position and 0.075 degrees in angular orientation. An optical component is machined from aluminum, aluminum alloys, stainless steel, nickel, copper or beryllium. The machining includes forming at least first, second and third cylindrical openings in the material, wherein the second and third cylindrical openings in the material are threaded. A cylindrical rod is positioned in the first cylindrical opening in the machined optical component, wherein the cylindrical rod extends away from a flat back surface of the optical component at an angle perpendicular to the flat back surface. A mount is provided having a flat front surface and at least first, second and third cylindrical openings that extend from the flat front surface into the mount at an angle perpendicular to the flat front surface. At least first and second of the plurality of cylindrical openings in the mount pass completely through a thickness of the mount, and first and second screws are respectively disposed in the first and second cylindrical openings in the mount. The first and second screws have an outer diameter that matches an inner diameter of the first and second cylindrical openings in the mount. Next, the mount is positioned with respect to the optical component by simultaneously aligning the metal rod extending from the optical component with the third opening in the mount, the second threaded opening in the optical component with the first opening in the mount, and third threaded opening in the optical component with the second opening in the mount. While the mount and the optical component are aligned, the cylindrical rod is pressed into the third cylindrical opening in the mount until the back surface of the optical component contacts the front surface of the mount. Following the inserting, friction between the cylindrical rod and the third opening in the mount inhibits rotation of the mount about an axis perpendicular to the front and back surfaces and tightness between the third cylindrical opening in the mount and the cylindrical rod restricts lateral movement of the mount with respect to the optical component. Thereafter, the first and second screws are rotated into the second and third threaded openings respectively in the optical component, whereby the mount is coupled to the optical component with said precision (i.e., at least 12.5 microns in position and 0.075 degrees in angular orientation.)
In accordance with a still further aspect, the present invention is directed to a method for forming a monolithic metal optical element. A mass of material (e.g., aluminum, aluminum alloys, stainless steel, nickel, copper or beryllium) is machined to form a monolithic component having a first face and a second face opposite the first face. The first face of the monolithic component comprises a focusing mirror or a collimating mirror. The machining is used to form a first cylindrical opening for receiving a cylindrical alignment rod that extends away from the second face at an angle perpendicular to a plane defined by the second face, a second cylindrical opening for receiving a first screw that extends away from the second face at an angle perpendicular to the plane defined by the second face, and a third cylindrical opening for receiving a second screw that extends away from the second face at an angle perpendicular to the plane defined by the second face. Alternatively, the second face of the optical element may be perpendicular to the first face, or any angle between parallel and perpendicular.
In accordance with yet a further aspect, the present invention is directed to a method for forming an optical grating element. A mass of material (e.g., aluminum, aluminum alloys, stainless steel, nickel, copper or beryllium) is machined to form a first face of the optical grating element, a first cylindrical opening that extends from the first face into the material at an angle perpendicular to the first face, a second cylindrical opening for receiving a first screw that extends from the first face into the material at an angle perpendicular to the first face, and a third cylindrical opening for receiving a second screw that extends from the first face into the material at an angle perpendicular to the first face. A cylindrical alignment rod is inserted into the first cylindrical opening, wherein, after the inserting, the cylindrical alignment rod extends away from the material at an angle perpendicular to the first face. A second face of the optical grating element is fabricated using an epoxy replication process, wherein the second face is perpendicular to the first face, the second face is formed from a resin layer bonded to the machined material, and the second face comprises an optical grating. Alternatively, the second face of the optical grating element may be parallel to the first face, or any angle between parallel and perpendicular.
Spectrometer 100 includes an entrance slit 110, a collimating mirror 120, a grating 130 and a focusing mirror 140. As shown in
As shown in
Referring now to
Referring now to
Referring now to
Referring now to
Referring again to
Substrate 300 has a flat upper surface 300 a that defines a further plane 300 b. Substrate 300 may be formed from any of the following materials: aluminum, aluminum alloys, stainless steel, nickel, copper, beryllium, titanium, aluminum composite, graphite or graphite composites. A cylindrical opening 302 extends from the upper surface 300 a of the substrate into substrate 300 at an angle perpendicular to plane 300 b. Threaded openings 304, 306 extend from the upper surface 300 a of the substrate into the substrate at an angle perpendicular to plane 300 b.
The mount 320 is positioned with respect to the substrate 300 by simultaneously aligning metal rod 330 with opening 302 in the substrate, opening 350 in the mount with threaded opening 304 in the substrate, and opening 352 in the mount with threaded opening 306 in the substrate. While the mount 320 and substrate 300 are aligned, rod 330 is inserted into the cylindrical opening 302 in the substrate until the bottom surface 320 a of the mount contacts the upper surface 300 a of the substrate. Following the inserting, friction between the rod 330 and opening 302 in the substrate inhibits rotation of mount 320 about an axis perpendicular to the planes 300 a, 320 a, and tightness between opening 302 in the substrate and rod 330 restricts lateral movement of mount 320 with respect to the substrate 300. After the inserting, screws 340, 342 are rotated into threaded openings 350, 352, respectively in the substrate, thereby coupling mount 320 to substrate 300 with a precision of at least 12.5 microns in position and 0.075 degrees in angular orientation.
Mount 320 has a flat front surface 320 c and openings 322, 324, 326 that extend from the flat front surface 320 c into the mount at an angle perpendicular to flat front surface 320 a. At least two of the openings 322, 324, 326 in the mount preferably pass completely through a thickness of the mount, and first and second screws (not shown) are respectively disposed in two of the cylindrical openings 322, 324, 326 in the mount. The first and second screws have an outer diameter that matches an inner diameter of openings 322, 324, 326 in the mount.
Next, the mount 320 is positioned with respect to the optical component 310 by simultaneously aligning the metal rod 370 extending from the optical component with opening 318 in the mount, threaded opening 312 in the optical component with the opening 322 in the mount, and threaded opening 314 in the optical component with opening 324 in the mount. While mount 320 and the optical component 310 are aligned, cylindrical rod 370 is pressed into the cylindrical opening 318 in the mount until the back surface 310 a of the optical component contacts the front surface 320 c of the mount. Following the inserting, friction between cylindrical rod 370 and opening 318 in the mount inhibits rotation of the mount 320 about an axis perpendicular to surfaces 310 a, 320 c, and tightness between cylindrical opening 318 in the mount and cylindrical rod 370 restricts lateral movement of the mount 320 with respect to the optical component 310. Thereafter, two screws (not shown) are rotated into the threaded openings 312, 314 respectively in the optical component, thereby coupling mount 320 to optical component 310 with a precision of at least 12.5 microns in position and 0.075 degrees in angular orientation.
Finally, it will be appreciated by those skilled in the art that changes could be made to the embodiments described above without departing from the broad inventive concept thereof. It is understood, therefore, that this invention is not limited to the particular embodiments disclosed, but is intended to cover modifications within the spirit and scope of the present invention as defined in the appended claims.
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|U.S. Classification||359/819, 356/305, 250/339.07|
|International Classification||G01N21/35, G01J3/28, G01J3/40, G02B7/02, G01J5/02, G01J3/02|
|Cooperative Classification||G01J3/0291, G01J3/0202, G01J3/0256, G01J3/02, G01J3/2803, G01N21/35, G01J3/0264|
|European Classification||G01J3/02R, G01J3/02A, G01J3/02E, G01J3/02C, G01J3/02, G01J3/28B|
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|Jul 17, 2015||REMI||Maintenance fee reminder mailed|
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